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A BGK-based Two-Equation Turbulence Model Algorithm for Solving Compressible Navier-Stokes Equations

机译:基于BGK的两方程湍流模型算法求解可压缩的Navier-Stokes方程

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The implementation and validation of the k-ε / k-ω SST (Shear-Stress-Transport) two-equation turbulence model into the existing BGK (Bhatnagaar-Gross-Krook) flow solver for compressible Navier-Stokes equations in two-space dimensions generalized coordinates are presented. In developing the desired algorithm, the convection flux terms are discretized by a semi-discrete finite difference method. Then, the resulting inviscid flux functions are approximated by the gas-kinetic BGK scheme based on the approximate collisional Boltzmann equation. For high-order spatial accuracy, the cell interface values required by the inviscid flux functions are reconstructed via the MUSCL (Monotone Upstream-Centered Schemes for Conservation Laws) variable interpolation method coupled with a minmod limiter. As for the diffusion flux terms, they are discretized with a second-order central difference scheme. An explicit-type time integration method known as the modified fourth-order Runge-Kutta method is used to march the solution to steady-state. Four test cases have been solved using the developed algorithm, namely turbulent flat plate, transitional flat plate, turbulent RAE2822 airfoil and turbulent Sajben diffuser flows. The accuracy of the solver is examined and results obtained from the computations are also compared with available experimental or analytical data that will demonstrate good agreement has been obtained.
机译:将k-ε/k-ωSST(剪切-应力-运输)两方程湍流模型实施和验证到现有的BGK(Bhatnagaar-Gross-Krook)流动求解器中以用于二维空间可压缩的Navier-Stokes方程提出了广义坐标。在开发所需算法时,对流通量项通过半离散有限差分法离散化。然后,基于近似碰撞玻耳兹曼方程,通过气体动力学BGK方案对所得的无粘性通量函数进行近似。为了获得高阶空间精度,无粘通量函数所需的像元界面值是通过MUSCL(守恒定律的单调上游中心方案)变量插值方法与minmod限制器一起重建的。至于扩散通量项,它们通过二阶中心差分方案离散化。一种显式时间积分方法,称为改进的四阶Runge-Kutta方法,用于使解决方案进入稳态。使用开发的算法已解决了四个测试案例,即湍流平板,过渡平板,湍流RAE2822机翼和湍流Sajben扩散器流。检查求解器的准确性,并将从计算中获得的结果与可用的实验或分析数据进行比较,这些数据将证明已获得良好的一致性。

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